[IGSREPORT-17920] Wk 1552 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Oct 22 05:01:50 PDT 2009
******************************************************************************
IGS Electronic Report 22 Oct 05:01:53 PDT 2009 Message Number 17920
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1552 (Oct 04, 2009 - Oct 10, 2009)
Contact: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the centers
absolute deviation to the unweighted average orbit after removing small
differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1552.
For long arc computations the Earth Orientation Parameters (EOPs) are fixed to
the values of the final IGS (GPS) combination.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
Weber R., 2000, IGS Technical Report 1999
PRODUCTS GENERATED:
-------------------
The combined IGL-ephemerides are written to daily files in the SP3-format.
The satellite accuracy codes in the header are based on the weighted rms.
for each satellite. Note, that the result files contain all satellites
that were analysed by at least one center. We refer to the 'REMARKS' section
below, in case a satellite or center was excluded from the combination.
The following naming convention is used for the result files:
igl1552[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1552 in the SP3 format.
igl15527.sum Combination Report for GPS Week 1552.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only.
3. Starting on 01-May-2005 (GPS Week 1321; MJD 53491)[IGSMAIL-5151]
BKG, ESA, and CODE will start to refer their GLONASS orbit products
to the following satellite antenna offset (SAO) values:
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets derived from the
bkg summary files were added to the broadcast clocks.
Day | applied clock offset
----+---------------------
0 | 238.9 ns
1 | 238.4 ns
2 | 233.0 ns
3 | 231.2 ns
4 | 207.2 ns
5 | 195.6 ns
6 | 140.7 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
1 | BKG | R23
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.1552, 1a.1552).
Table 2 contains the complete ephemeris and clock correction transformation
parameters (includes both the apriori and a posteriori values) for each
centre and each day (Tables 2.1552.0-6)
Table 3 contains two types of daily RMS for each satellite and centre, along
with the computed satellite position sigmas for the combined orbits
(tables 3.1552.0-6).
The first type of satellite RMS is based on orbit combination and the
second RMS type is a result of the 7-day arc evaluation of each centre
ephemerides.
Table 1: Week 1552 summary. (Oct 04, 2009 - Oct 10, 2009)
Table 1.1552.a GPS week : 1552 MJD: 55108.0-55114.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 102| 0 0 -1 17 6 51 -.18 32 28 | 0 -302 4911 5592
| 1 2 5 22 14 139 .08 | 0 1444
cod 224| -1 0 -1 19 -15 51 -.12 15 15 | --- --- --- ---
| 1 1 2 19 26 35 .02 | --- ---
esx 125| 0 -1 2 -10 11 -57 .44 23 21 | 131797 6655 6447 13116
| 1 2 2 38 29 50 .06 | 19811 12500
iac n/a| 0 1 0 -46 -2 -77 -.16 26 26 | 215717 41 6437 13311
| 2 1 6 32 31 93 .08 | 33527 8403
mcc n/a| 1 8 13 -42 -45 307 .13 122 122 | --- --- --- ---
| 10 10 12 105 81 547 .29 | --- ---
Table 1.1552.b GPS week : 1552 MJD: 55108.0-55114.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R02 | 8 14 11 8 12 17 9 |
R03 | 11 12 12 10 9 10 8 |
R07 | 12 15 13 8 12 9 11 |
R08 | 11 9 12 10 14 13 17 |
R10 | 11 12 14 12 12 15 11 |
R11 | 9 15 12 14 16 22 16 |
R13 | 10 11 12 8 12 19 13 |
R14 | 8 9 10 12 16 12 18 |
R15 | 10 13 12 11 10 9 12 |
R17 | 13 14 13 15 11 11 15 |
R18 | 9 10 9 9 10 9 10 |
R19 | 10 13 9 7 10 11 10 |
R20 | 13 10 11 10 9 11 14 |
R21 | 11 18 13 11 9 9 15 |
R23 | 32 15 37 15 21 17 13 |
R24 | 22 12 15 17 17 15 16 |
Table 1.1552.c GPS week : 1552 MJD: 55108.0-55114.0
Daily transformation of broadcast orbits (brd) to the combined IGL orbit.
Mean and standard deviations of the transformation parameters for the
whole gpsweek.
CEN WEEK DAY | DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm] | [ps] [ps/d]
-------------+------------------------------------------------------------+----------------
brd 1552 0 | 31 60 221 19 -1794 -15070 90.0 2785 2785 | 238862 0
brd 1552 1 |10560 ---- -3756 -28200 -26040 218100 <<<< >>>>> >>>>> | 238419 0
brd 1552 2 | 15 98 135 -2574 1300 -13550 92.5 2435 2435 | 233040 0
brd 1552 3 | 142 -103 166 -284 1488 -11310 87.3 2130 2130 | 231238 0
brd 1552 4 | -86 -5 224 -2916 -727 -3620 88.9 1584 1584 | 207179 0
brd 1552 5 | 21 143 96 -2740 -2146 -4510 88.2 3609 3609 | 195638 0
brd 1552 6 | 4 96 292 -162 -973 -10260 88.4 2624 2624 | 140652 0
-------------+------------------------------------------------------------+----------------
brd 1552 mean| 1526 -4034 -373 -5265 -4127 22825 54.6 >>>>> >>>>> | 212146 0
brd 1552 sdev| 3983 10801 1492 10197 9764 86214 91.6 >>>>> >>>>> | 35622 0
Table 2: Daily transformation of each centre to the combined IGL orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1552.0 GPS week: 1552 Day: 0 MJD: 55108
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 102| -1 0 -2 13 3 -44 -.31 35 24 | 0 2109 3357 3811
cod 224| -1 0 1 59 -46 96 -.14 15 14 | --- --- --- ---
esx 125| 1 0 5 -54 30 5 .52 21 18 | 141084 -1143 4903 10578
iac n/a| 4 0 -6 -46 2 -144 -.26 25 25 | 241771 -2064 4898 10184
mcc n/a| 1 17 33 -161 -71 701 -.39 116 116 | --- --- --- ---
Table 2.1552.1 GPS week: 1552 Day: 1 MJD: 55109
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 102| 0 3 -4 12 22 251 -.21 48 50 | 0 855 2722 3195
cod 224| -1 -1 -1 8 27 59 -.12 16 17 | --- --- --- ---
esx 125| 1 -4 2 -5 -19 -134 .46 23 20 | 148379 -1527 4970 12718
iac n/a| 0 2 0 -69 -16 -238 -.16 25 25 | 237547 -1753 4953 12367
mcc n/a| -14 2 18 -20 -170 -284 -.01 119 119 | --- --- --- ---
Table 2.1552.2 GPS week: 1552 Day: 2 MJD: 55110
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 102| -2 0 -11 65 -2 196 -.13 39 28 | 0 122 5878 6942
cod 224| 0 0 -4 1 -12 22 -.11 16 15 | --- --- --- ---
esx 125| 0 0 2 -67 0 -111 .35 23 22 | 135761 7970 7478 12982
iac n/a| 0 0 12 -8 9 -78 -.03 25 25 | 232808 2237 7451 13129
mcc n/a| 4 -8 -2 60 8 50 .43 108 108 | --- --- --- ---
Table 2.1552.3 GPS week: 1552 Day: 3 MJD: 55111
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 102| 1 -1 -3 25 28 79 -.18 20 19 | 0 -1960 6478 7251
cod 224| 0 1 -2 10 -46 1 -.09 13 13 | --- --- --- ---
esx 125| -1 -2 2 -7 -8 -54 .46 23 21 | 147607 6362 7701 17170
iac n/a| -2 1 2 -61 55 -59 -.26 24 24 | 232841 -891 7718 18070
mcc n/a| 6 0 8 -139 64 175 .13 100 100 | --- --- --- ---
Table 2.1552.4 GPS week: 1552 Day: 4 MJD: 55112
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 102| -1 3 3 -5 9 8 -.15 23 20 | 0 -1471 8729 9663
cod 224| 0 0 0 28 -20 81 -.15 17 17 | --- --- --- ---
esx 125| 0 -2 4 32 24 -27 .39 22 19 | 132451 33458 10496 21920
iac n/a| -2 4 -6 -99 3 -41 -.16 26 26 | 210039 17328 10530 22666
mcc n/a| 5 16 8 -135 22 -289 .23 95 95 | --- --- --- ---
Table 2.1552.5 GPS week: 1552 Day: 5 MJD: 55113
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 102| 0 -2 5 8 -10 27 -.07 28 24 | 0 -442 3933 4696
cod 224| 0 0 -3 15 -2 24 -.12 14 13 | --- --- --- ---
esx 125| 0 1 -2 29 65 -17 .42 25 23 | 126761 3856 4322 8098
iac n/a| 0 -1 0 -18 -39 -36 -.15 30 30 | 209540 -8732 4245 8211
mcc n/a| 14 14 4 108 -100 621 .05 150 150 | --- --- --- ---
Table 2.1552.6 GPS week: 1552 Day: 6 MJD: 55114
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 102| 0 -1 0 4 -3 -155 -.23 28 27 | 0 -1332 3285 3590
cod 224| -4 1 0 10 -5 77 -.09 15 14 | --- --- --- ---
esx 125| 4 0 2 -2 -9 -60 .45 27 26 | 90537 -2391 5260 8350
iac n/a| 0 0 -1 -19 -34 57 -.12 24 24 | 145479 -5838 5270 8555
mcc n/a| -10 13 21 -5 -69 1175 .48 169 169 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGL column gives resulting satellite accuracy measures found in
SP3 header. The last IGL column gives the RMS fit of the IGL orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGL orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1552.0 GPS week: 1552 Day: 0 MJD: 55108
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 883 17 11 9 16 --- 7 | 18 37 37 23 --- 28
R03 | 2202 23 12 18 23 --- 10 | 21 41 48 47 --- 38
R07 | 5116 12 23 15 24 --- 11 | 32 42 35 30 --- 31
R08 | 2053 16 19 19 22 149 11 | 19 33 35 23 94 24
R10 | 1083 22 10 23 19 --- 10 | 40 33 33 42 --- 33
R11 | 3439 19 9 17 15 121 8 | 36 46 54 39 50 42
R13 | 1284 22 14 19 15 --- 10 | 50 52 52 51 --- 50
R14 | 1892 13 14 13 17 --- 8 | 28 25 36 29 --- 27
R15 | 6368 21 12 18 16 56 9 | 45 49 35 43 55 40
R17 | 896 26 14 22 29 --- 13 | 60 56 63 83 --- 63
R18 | 658 13 10 14 21 --- 8 | 24 25 37 33 --- 27
R19 | 1016 20 11 14 21 --- 9 | 27 32 46 42 --- 34
R20 | 2168 28 13 22 24 --- 12 | 27 34 50 40 --- 36
R21 | 691 20 11 14 30 --- 11 | 45 46 54 47 --- 46
R23 | 3726 104 24 42 44 --- 32 | 60 94 102 117 --- 90
R24 | 2815 55 27 35 38 --- 22 | 216 187 173 197 --- 189
------+------------------------------------+--------------------------------
RMS | 2784 35 15 21 25 116 |T 46 52 55 55 66 49
WRMS | 2784 24 14 18 25 116 |NE 46 52 55 55 66 49
MEDI | 1892 20 12 18 21 121 |MD 32 41 46 42 55 36
Table 3.1552.1 GPS week: 1552 Day: 1 MJD: 55109
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 18 20 27 30 --- 14 | 21 26 49 34 --- 28
R03 |>>>>> 16 20 13 28 --- 11 | 35 35 35 35 --- 33
R07 |>>>>> 21 23 20 38 --- 15 | 28 28 48 36 --- 32
R08 |>>>>> 15 13 12 21 122 9 | 33 27 41 19 70 27
R10 |23348 25 18 22 16 --- 12 | 28 35 39 32 --- 29
R11 |>>>>> 32 10 36 19 146 15 | 38 30 45 25 55 29
R13 |>>>>> 22 14 20 19 --- 10 | 68 60 58 71 --- 62
R14 |>>>>> 13 15 17 18 --- 9 | 30 30 31 26 --- 25
R15 |>>>>> 24 16 19 29 78 12 | 33 27 32 31 33 26
R17 |>>>>> 31 14 28 20 --- 13 | 48 62 64 62 --- 56
R18 |>>>>> 16 17 18 17 --- 10 | 35 21 42 25 --- 27
R19 |>>>>> 31 14 11 29 --- 12 | 32 24 29 40 --- 25
R20 |>>>>> 17 11 15 26 --- 10 | 22 21 22 22 --- 17
R21 |>>>>> 37 17 42 22 --- 17 | 41 55 76 44 --- 50
R23 |>>>>> 169 13 24 26 --- 15 | 53 57 63 71 --- 65
R24 |>>>>> 24 18 17 24 --- 12 | 172 182 182 167 --- 175
------+------------------------------------+--------------------------------
RMS |>>>>> 48 16 23 25 118 |T 44 45 53 46 52 44
WRMS |>>>>> 50 17 20 25 118 |NE 44 45 53 46 52 44
MEDI |>>>>> 22 15 19 22 122 |MD 33 30 42 34 55 29
Table 3.1552.2 GPS week: 1552 Day: 2 MJD: 55110
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1119 22 20 18 17 --- 11 | 18 27 25 25 --- 18
R03 | 1189 30 11 22 22 --- 12 | 18 36 47 39 --- 35
R07 | 6018 20 12 23 32 --- 12 | 21 29 42 23 --- 26
R08 | 870 31 19 16 12 107 11 | 16 42 37 39 49 31
R10 | 2371 33 11 29 27 --- 14 | 33 44 46 41 --- 38
R11 | 2425 21 17 27 20 139 12 | 27 37 52 40 39 37
R13 | 1699 26 15 24 18 --- 11 | 42 37 42 33 --- 34
R14 | 2276 16 14 20 18 --- 9 | 20 22 43 29 --- 26
R15 | 955 20 12 17 31 63 11 | 31 39 45 38 46 36
R17 | 2155 32 9 25 22 --- 12 | 57 70 86 76 --- 71
R18 | 2776 17 13 15 18 --- 9 | 31 25 31 26 --- 23
R19 | 1290 13 14 16 20 --- 9 | 33 33 48 48 --- 38
R20 | 1806 16 15 25 19 --- 11 | 23 29 45 27 --- 27
R21 | 2210 16 15 28 25 --- 12 | 24 32 34 28 --- 26
R23 | 3258 130 29 29 48 --- 36 | 53 57 58 74 --- 52
R24 | 1403 22 18 29 32 --- 14 | 176 180 162 174 --- 173
------+------------------------------------+--------------------------------
RMS | 2435 39 16 23 25 108 |T 38 46 52 47 44 43
WRMS | 2435 28 15 22 25 108 |NE 38 46 52 47 44 43
MEDI | 1806 21 14 23 20 107 |MD 27 36 45 38 46 34
Table 3.1552.3 GPS week: 1552 Day: 3 MJD: 55111
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 852 11 9 16 21 --- 8 | 29 37 51 36 --- 37
R03 | 1006 15 10 24 22 --- 10 | 28 34 32 21 --- 25
R07 | 5335 14 12 16 13 --- 8 | 33 45 42 50 --- 41
R08 | 1510 19 14 18 17 97 9 | 50 50 44 48 33 45
R10 | 2191 18 16 17 30 --- 11 | 25 48 37 47 --- 38
R11 | 924 21 14 36 27 137 14 | 33 39 66 40 39 39
R13 | 989 14 8 15 16 --- 7 | 66 73 75 64 --- 70
R14 | 2701 17 14 23 33 --- 12 | 27 31 36 35 --- 25
R15 | 1063 21 11 22 23 45 11 | 24 39 51 46 39 38
R17 | 2228 28 7 40 23 --- 14 | 45 54 70 64 --- 52
R18 | 1839 18 11 15 22 --- 9 | 42 33 47 33 --- 35
R19 | 1113 16 9 12 13 --- 7 | 27 30 35 27 --- 27
R20 | 1397 19 8 18 20 --- 9 | 29 28 32 28 --- 26
R21 | 2289 20 17 16 23 --- 11 | 31 48 46 41 --- 40
R23 | 2444 29 17 27 32 --- 14 | 95 69 93 95 --- 78
R24 | 1511 33 25 25 37 --- 17 | 131 144 141 130 --- 136
------+------------------------------------+--------------------------------
RMS | 2130 20 13 23 24 100 |T 44 50 56 50 37 47
WRMS | 2130 19 13 21 24 100 |NE 44 50 56 50 37 47
MEDI | 1510 18 11 18 22 97 |MD 31 39 46 41 39 38
Table 3.1552.4 GPS week: 1552 Day: 4 MJD: 55112
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2431 20 21 18 21 --- 11 | 18 34 36 22 --- 22
R03 | 816 17 14 10 21 --- 9 | 18 23 26 18 --- 19
R07 | 2581 21 15 26 17 --- 11 | 38 32 58 48 --- 39
R08 | 1915 34 19 13 27 98 13 | 18 30 31 36 19 21
R10 | 797 12 18 17 30 --- 11 | 45 45 49 70 --- 49
R11 | 1341 28 16 38 23 128 15 | 45 48 37 49 44 40
R13 | 908 23 15 18 23 --- 11 | 55 66 67 73 --- 63
R14 | 1640 18 29 20 39 --- 16 | 23 20 32 41 --- 20
R15 | 1214 18 9 13 26 33 9 | 23 27 26 47 78 26
R17 | 1202 17 15 16 24 --- 10 | 48 55 54 77 --- 56
R18 | 1436 16 13 12 24 --- 9 | 18 19 26 49 --- 23
R19 | 579 15 12 22 13 --- 9 | 36 41 63 46 --- 44
R20 | 1223 17 10 17 19 --- 9 | 33 30 41 23 --- 28
R21 | 1429 17 12 11 22 --- 9 | 19 34 32 37 --- 27
R23 | 999 42 15 45 43 --- 21 | 67 68 74 103 --- 73
R24 | 2728 33 25 26 29 --- 16 | 168 166 150 165 --- 159
------+------------------------------------+--------------------------------
RMS | 1584 23 17 22 26 95 |T 42 46 50 56 47 44
WRMS | 1584 20 17 19 26 95 |NE 42 46 50 56 47 44
MEDI | 1223 18 15 17 23 98 |MD 33 34 37 47 44 28
Table 3.1552.5 GPS week: 1552 Day: 5 MJD: 55113
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |12762 19 18 47 26 --- 16 | 20 33 67 24 --- 34
R03 | 911 20 11 22 18 --- 10 | 16 24 32 17 --- 19
R07 | 3485 16 11 9 23 --- 8 | 35 35 39 31 --- 33
R08 | 1819 27 20 14 25 49 12 | 30 29 40 44 21 29
R10 | 1303 30 15 21 39 --- 14 | 23 47 41 49 --- 38
R11 | 1890 54 11 46 42 141 21 | 42 55 83 52 41 55
R13 | 720 37 23 28 44 --- 18 | 84 110 105 99 --- 97
R14 | 2882 28 9 22 29 --- 12 | 38 20 36 49 --- 29
R15 | 1234 23 9 14 21 212 9 | 17 32 33 37 63 26
R17 | 1079 16 8 21 28 --- 10 | 24 39 55 33 --- 35
R18 | 804 20 8 19 17 --- 9 | 17 21 29 27 --- 19
R19 | 805 28 9 21 17 --- 11 | 25 24 29 29 --- 22
R20 | 1672 15 13 23 22 --- 10 | 22 23 34 28 --- 21
R21 | 721 12 12 18 19 --- 8 | 23 33 30 20 --- 23
R23 | 1491 43 16 15 45 --- 17 | 58 77 89 98 --- 76
R24 | 2375 26 18 23 39 --- 15 | 131 137 134 125 --- 131
------+------------------------------------+--------------------------------
RMS | 3609 28 14 25 30 149 |T 37 46 54 47 41 42
WRMS | 3609 24 13 23 30 149 |NE 37 46 54 47 41 42
MEDI | 1303 23 11 21 25 141 |MD 24 33 39 33 41 29
Table 3.1552.6 GPS week: 1552 Day: 6 MJD: 55114
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1813 21 11 16 18 --- 9 | 18 31 39 23 --- 24
R03 | 919 9 11 17 18 --- 8 | 18 32 35 22 --- 25
R07 | 6392 24 13 21 20 --- 11 | 26 35 41 30 --- 30
R08 | 1771 28 19 35 37 45 16 | 18 36 43 34 35 25
R10 | 2666 12 16 11 29 --- 10 | 45 47 54 66 --- 51
R11 | 1937 45 12 29 23 148 16 | 43 56 49 53 40 49
R13 | 1272 17 17 33 24 --- 13 | 97 120 130 96 --- 111
R14 | 4012 53 13 31 27 --- 18 | 32 22 41 31 --- 24
R15 | 2015 21 15 27 19 249 11 | 42 48 55 63 52 50
R17 | 1352 23 19 30 31 --- 14 | 41 59 50 66 --- 53
R18 | 1099 19 8 24 18 --- 10 | 18 21 31 33 --- 21
R19 | 1018 24 13 11 21 --- 10 | 31 27 32 34 --- 28
R20 | 1063 29 18 28 20 --- 13 | 23 27 42 22 --- 23
R21 | 1366 22 18 44 15 --- 15 | 25 35 30 23 --- 25
R23 | 1381 21 17 25 24 --- 12 | 86 99 98 114 --- 98
R24 | 4517 38 16 25 34 --- 16 | 155 156 144 157 --- 152
------+------------------------------------+--------------------------------
RMS | 2624 28 15 27 24 169 |T 44 53 57 54 42 49
WRMS | 2624 27 14 26 24 169 |NE 44 53 57 54 42 49
MEDI | 1381 22 15 25 21 148 |MD 31 35 42 34 40 28
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